Portable generator and air compressor mounting arrangement

ABSTRACT

A system, in one embodiment, may include a chassis, an engine coupled to the chassis, a generator coupled to the engine, and a rotary screw compressor coupled to the chassis independent from the engine. The engine may be configured to drive both the generator and the rotary screw compressor. A method, according to another embodiment, may include isolating a rotary air compressor from an engine and a generator in a common chassis. The isolating may include separately mounting the rotary air compressor and the engine with a resilient or distance adjustable connection in between. The isolating also may include resiliently mounting the engine, or the rotary air compressor, or both.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a Continuation Application of U.S. patentapplication Ser. No. 11/742,311, entitled “Portable Generator and AirCompressor Mounting Arrangement”, filed Apr. 30, 2007, which is hereinincorporated by reference in its entirety for all purposes.

BACKGROUND

The invention relates generally to welding systems and more particularlyto welding systems utilizing an engine coupled to an air compressor andwelding generator in a single unit.

Welding systems generally use an electrical current (e.g., weldingcurrent) to perform welding. The electrical current may be provided byan electrical power source (such as a power grid or battery) or anelectrical generator coupled to a mechanical power source. Examples ofmechanical power sources include engines that output power via arotating drive shaft. Typically, the drive shaft is coupled to otherdevices that consume the energy provided by the rotating drive. Forinstance, welding systems often include internal combustion engines(such as gas or diesel engines) and an alternator or generatorconfigured to convert the mechanical energy generated by the engine intoelectrical energy (e.g., electrical current). These systems are oftenreferred to as engine-driven welding generators. An advantage of anengine-driven system is the potential portability of the system. Forinstance, welding systems that employ a generator coupled to an engineare typically configured as standalone units that do not haveconnections to a supplemental power source, such as a power grid. Thismay be useful for systems that are traditionally operated at remoteworksites.

In addition to needing a source of welding current at a worksite,welding operators often desire other outputs to more efficientlycomplete a job. For example, a welding operator may also use compressedair to operate plasma cutters, air tools and the like. Typically,compressed air is provided via a standalone air supply. Thus, a weldingoperator may use, both, a standalone engine-driven welding generator anda standalone air supply. The independence of the two units may increasethe amount of time and labor involved with setup, transportation, and soforth. In addition, the independence of the two units may result in anincreased amount of maintenance and repair costs due to duplication ofparts.

BRIEF DESCRIPTION

A system, in one embodiment, may include a chassis, an engine coupled tothe chassis, a generator coupled to the engine, and a rotary screwcompressor coupled to the chassis independent from the engine. Theengine may be configured to drive both the generator and the rotaryscrew compressor.

A method, according to another embodiment, may include isolating arotary air compressor from an engine and a generator in a commonchassis. The isolating may include separately mounting the rotary aircompressor and the engine with a resilient or distance adjustableconnection in between. The isolating also may include resilientlymounting the engine, or the rotary air compressor, or both.

DRAWINGS

These and other features, aspects, and advantages of the presentinvention will become better understood when the following detaileddescription is read with reference to the accompanying drawings in whichlike characters represent like parts throughout the drawings, wherein:

FIG. 1 is a partial perspective view of an exemplary engine-drivenwelding generator/compressor system, wherein two top access panels arerotated to open positions and a side access panel is removed to revealvarious internal features in accordance with embodiments of the presentinvention;

FIG. 2 is another partial perspective view of the weldinggenerator/compressor system as illustrated in FIG. 1, wherein an entiretop access panel assembly is removed to further illustrate variousinternal features in accordance with embodiments of the presentinvention;

FIG. 3 is a side view of the welding generator/compressor system asillustrated in FIG. 1, wherein the two top access panels are rotated toclosed positions and the side access panel is removed to furtherillustrate various internal features in accordance with embodiments ofthe present invention;

FIG. 4 is a diagram illustrating an exemplary embodiment of the weldinggenerator/compressor system as illustrated in FIGS. 1-3;

FIG. 5 is a diagram illustrating an exemplary embodiment of a belttensioner of the welding generator/compressor system as illustrated inFIGS. 1-4; and

FIG. 6 is a diagram illustrating an alternate embodiment of the belttensioner of the welding generator/compressor system as illustrated inFIGS. 1-5.

DETAILED DESCRIPTION

Referring now to the drawings, FIGS. 1-3 illustrate an engine-drivenwelding generator/compressor system 10 having an engine 12 drivinglycoupled to a welding generator 14 and an air compressor 16 in a singleenclosure 18 in accordance with an exemplary embodiment of the presenttechnique. FIG. 1 is a partial perspective view of the system 10 withside access panels removed and top access panels or hatches rotated toopen positions. FIG. 2 is another partial perspective view of the system10 as illustrated in FIG. 1, wherein the entire top access panelassembly is removed to provide a better view of the internal features ofthe system 10. FIG. 3 is a side view of the system 10 as illustrated inFIGS. 1 and 2. As depicted, the system 10 is configured to providemultiple outputs, including welding current, alternating current (AC)power, and compressed air.

As discussed in detail below, the illustrated system includes a varietyof features to improve serviceability, reliability, controllability, andintegration of the air compressor 16 within the single enclosure 18 ofthe system 10. For example, the illustrated system 10 may include a topside oil fill to enable access at the top of the system 10, rather thana lower or more inaccessible oil fill location. The illustrated system10 also may include unique control features, such as a load prioritycontrol configured to monitor various loads (e.g., generator 14,compressor 16, external loads, etc.) on the engine 12, identify possibleoverload conditions, and adjust the various loads based on prioritylevels. The control features also may include a specific air compressorload control, which may be configured to reduce the engine speed and/orgradually engage (e.g., via a clutch) the air compressor 16 during startup (e.g., a soft start control). Furthermore, the control features mayinclude a specific air compressor control regulator, which may bemounted directly on a control panel (e.g., a front panel) of the system10 rather than being in an inaccessible position well within the system10. The system 10 also may include a battery and/or a battery chargesystem, which may include features to monitor conditions of the battery(e.g., internal or external to the system 10) and to adjust thecharacteristics of the charge (e.g., variable output level, duration,etc.).

In certain embodiments, the system 10 may be described as an air packwelding system (e.g., AIRPAK). The engine 12 provides output power(e.g., a mechanical output) to drive both the welding generator 14 andthe air compressor 16. In the illustrated embodiment, the generator 14is coupled to one side of the engine 12, while the compressor 16 isindependently coupled to an opposite side of the engine 12. Thus, theengine 12 is sandwiched between the generator 14 and the compressor 16.In addition, the engine 12 may be mounted independently from thecompressor 16, such that the two are mechanically isolated from oneanother. As discussed in further detail below, the isolation between thecompressor 16 and the engine 12 may be addressed with a suitableengine-to-compressor coupling system, such as a geometrically adjustablecoupling. The geometrically adjustable coupling may include a tensioningsystem coupled to a belt and pulley system, a special resilient orspring-like belt, a clutch, or a combination thereof, to provide somedegree of flexibility, positional adjustability, or play. Thus, thegeometrically adjustable coupling is configured to maintain a connectionbetween the compressor 16 and the engine 12 despite variations indistance, vibrations, and so forth. In other words, the geometricallyadjustable coupling provides a resilient or distance adjustableconnection between the engine 12 and the compressor 16

As described below, the power from the engine 12 operates both thegenerator 14 and the air compressor 16 via a first shaft 20 and a secondshaft 22 (e.g., stub shaft), respectively. In some embodiments, theseshafts 20 and 22 may be independent from one another, while in otherembodiments shafts 20 and 22 may be part of a single shaft extendingthrough the engine 12. As illustrated, the shafts 20 and 22 extend outof opposite sides of the engine 12. These shafts 20 and 22 may bedirectly or indirectly coupled to one or more driven mechanisms. Forexample, an indirect coupling may include a belt and pulley system, agear system, or a chain and sprocket system. In the present embodiment,the first shaft 20 couples directly to the generator 14, while thesecond stub shaft 22 couples indirectly to the compressor 16. However,either arrangement can be used for the connection between the engine 12and the generator 14 and/or the compressor 16.

For example, as will be discussed in greater detail below, the engine 12is coupled to the compressor 16 via a belt and pulley system includingthe stub shaft 22, a pulley 24 coupled to the shaft 22, a compressordrive shaft 26 coupled to the compressor 16, a compressor pulley 28coupled to the shaft 26, and a drive belt 30 extending about the pulleys24 and 28. Therefore, the engine 12 is capable of providing power to thegenerator 14 and the air compressor 16 simultaneously. In theillustrated embodiment, the engine 12 rotates the stub shaft 22 totransmit rotation and torque via the pulleys 24 and 28 and drive belt 30to the compressor drive shaft 26 coupled to the air compressor 16.Accordingly, the mechanical energy generated by the engine 12 operatesthe air compressor 16. As discussed in detail below, in certainembodiments, the air compressor 16 includes a rotary screw compressor.Thus, the air compressor 16 and the system 10 may be capable ofcontinuously providing large volumes of compressed air 16 to a desiredapplication, such as a welding application, without any need for anintermediate storage tank.

As discussed in further detail below with reference to FIGS. 4-6, anembodiment of the system 10 includes a belt tensioner 68 that reducesslack in the drive belt 30 and maintains tension to transfer torque fromthe stub shaft 22 to the air compressor 16. Moreover, the belt tensioner68 may provide for simplified mounting of the drive belt 30 andcompensating for misalignment of the engine 12, the stub shaft 22,and/or the compressor drive shaft 26. For example, the belt tensioner 68may reduce stresses due to vibrations, wear and assembly. Furthermore,embodiments include isolating the engine 12 from other components viaisolators 86. The isolators 86 may be configured reduce the transmissionof vibrations from the engine 12 to the other components in the systemand/or may reduce the stresses of misalignments due to wear andassembly.

Returning to FIGS. 1-3, the engine 12 includes a power source configuredto provide power to the generator 14 and the air compressor 16. In anembodiment, the engine 12 may include a combustion engine powered bygas, diesel, LP fuel, natural gas, or other fuel, and driving one ormore drive shafts, e.g., 20 and 22. For example, the engine 12 mayinclude an industrial gas/diesel engine configured to output anywherefrom about 24 horsepower (Hp) to about 64 Hp. Generally, the weight ofsuch an engine 12 may vary with the size and Hp rating of the engine.For example, a 64 Hp diesel engine driven unit may weigh approximately1900 lbs., whereas a similar 24 Hp gasoline engine driven unit may weighless than approximately 1000 lbs. Thus, the portable system 10 maybenefit from the use of a smaller engine 12.

As discussed previously, embodiments may include a generator 14 coupledto the engine 12. Thus, the generator 14 may convert the power output(e.g., mechanical energy) of the engine 12 to electrical power.Generally, the generator 14 includes a device configured to convert arotating magnetic field into an electrical current (e.g., AC generator).The generator 14 includes a rotor (rotating portion of the generator)and a stator (the stationary portion of the generator). For example, therotor of the generator 14 may include the rotating drive shaft 20disposed in a single stator configured to create an electrical current(e.g., welding current) from the rotation of the magnetic field. In anembodiment, the generator may include a four-pole rotor and three-phaseweld output configured to provide beneficial welding characteristics.Further, the generator 14 may include a plurality of independent windingsections in the rotors and/or stators, such that the generator 14 isconfigured to output multiple electrical outputs having differentcharacteristics. For example, the generator 14 may include a firstsection configured to drive a welding current to a welder and a secondsection configured to drive a current for other AC outputs. As suggestedabove, multiple generators 14 may be connected to the drive shaft 20 orstub shaft 22.

Also coupled to the engine 12, the air compressor 16 may provide acontinuous source of compressed air for use in plasma cutting, pneumatictools, inflating a tire, blowing-off/cleaning a work piece, and thelike. For example, a welding operator may use compressed air as a highspeed gas ejected from the nozzle of a plasma torch, or may usecompressed air to operate tools, such as pneumatic impact wrenches,pneumatic spray guns, pneumatic lifts, and pneumatic air chisels. In theillustrated embodiment, the air compressor 16 may be described as acontinuous air supply compressor, an indirect mount air compressor, orboth. For example, certain embodiments of the system 10 use a type ofthe compressor 16 that is not a piston-type air compressor mounteddirectly to the engine 12. In an embodiment, the air compressor 16 mayinclude a rotary screw compressor or another suitable compressor 16configured to supply a continuous flow of compressed air without theneed for an intermediate storage tank.

Rotary screw compressors may include a type of gas compressor that has arotary type positive displacement mechanism. The rotary screw compressortypically includes one or more screws, which rotate within an enclosureto gradually shrink a series of passages defined by threads of thescrews and the surrounding enclosure. For example, the rotary screwcompressor may include a plurality (e.g., pair) of counter rotatingscrews, which intermesh with one another to progressively reduce airvolumes between the intermeshed threads (e.g., a series of shrinkingvolumes of air). For example, air is drawn in through an inlet port inthe enclosure, the gas is captured in a cavity, the gas is compressed asthe cavity reduces in volume, and the gas is finally discharged throughanother port in the enclosure. The design of a rotary screw aircompressor 16 generally provides for high volumes of compressed gas in acontinuous manner without the need for an intermediate storage tank.

Accordingly, the rotary screw air compressor 16 may provide a directsupply of compressed air on-demand to a desired application. Forexample, a plasma cutter may consume air directly from the unit withoutthe air being compressed into a tank, as generally done by piston-drivenair compressors. However, an embodiment including a rotary screw aircompressor 16 may include an air tank configured to store the compressedair. For example, a user may want to generate air for a given period andstore the compressed air for a later use.

Further, the rotary screw air compressor 16 may be configured to operateat high speeds and, thus, may use less gearing and space to couple therotary screw air compressor 16 to the engine 12. For example, in anembodiment, the system 10 may include a rotary screw air compressor 16operating at speed near the engine speed, such as 4000 rpm. Thus, thepulley 24 and the compressor pulley 18 may include similar 1 to 1 ratiosand not use a significantly larger compressor pulley 28 to step down theengine speed to accommodate the air compressor 16.

The system 10 may also have an oil fill assembly 31 that enables a userto perform regular maintenance on the air compressor 16. For example, asdepicted, the oil fill assembly 31 may include a configuration toprovide improved access to components of the air compressor 16 that mayotherwise be obscured by other devices within the system 10. Accordinglya user may easily check and add fluids to the air compressor 16. Forexample, the oil fill assembly 31 may be described as an extension,add-on, or retrofit system configured to relocate the oil fill locationfrom well within the system 10 to a top access location.

The system 10 may also include control circuitry to coordinate functionsof a plurality of devices. For example, as depicted in FIGS. 1-3, thesystem 10 includes control circuitry 32 in the vicinity of a controlpanel 34. In an embodiment, the control circuitry 32 may include aprocessor, memory, and software code configured to control and orcoordinate operation of the system 10. For example, the controlcircuitry 32 may monitor and control the speed and load on the engine12, the electrical output and loads on the generator 14, the air outputand loads on the compressor 16, the startup procedures (e.g., soft startof compressor 16), and/or the like. For example, as mentioned above, thecontrol circuitry 32 may identify an overload condition in response tosensed data, and then reduce the output to protect the system 10. Thecontrol circuitry 32 also may reduce the engine speed, graduallyincrease the engine speed, and/or gradually engage a clutch during startup of the compressor 16. The control circuitry 32 also may automaticallyadjust the outputs (e.g., compressed air output or electrical output)based on default or user defined priority levels, minimum workout outputlevels, maximum output levels, safety features, and so forth. Thecontrol circuitry 32 also may adjust output levels (e.g., compressed airoutput or electrical output) based on a particular application, sensedfeedback, and other closed-loop controls. For example, the controlcircuitry 32 may gradually decrease an electrical output for a batterycharging procedure based on sensed feedback from the battery, therebymaximizing the charge without overcharging the battery.

As depicted in FIGS. 1-3, the enclosure 18 includes a common base orframe 36 with various access panels to enable servicing, repair, and soforth. For example, a pair of side access panels (removed) is configuredto attach to opposite sides of the frame 36. A top 37 of the enclosure18 includes first and second access panels or hatches 38 and 39, whichare both rotatable between open and closed positions above thecomponents of the system 10. As illustrated, the first hatch 38 canrotate open to enable access to the compressor 16, the oil fill assembly31, and other features. The second hatch 39 can rotate open to enableaccess to the engine 12 and other features.

As depicted, the control panel 34 is coupled to an end of the enclosure18 near the generator 14. The control panel 34 may include variouscontrol inputs, indicators, displays, electrical outputs, air outputs,and so forth. In an embodiment, a user input 40 may include a knob orbutton configured for a mode of operation, an output level or type, etc.For instance, the user input 40 may include a dial to select a mode ofoperation, such as a DC weld, an AC weld, a battery charge, or an airtool operation. Other embodiments may include routing air from thecompressor 16 out of other location within the system 10, such a sideproximate to the air compressor 16. The control panel 34 may alsoinclude various indicators 42 to provide feedback to the user. Forexample, the indicator 42 may include an LCD, LED, or Vacuum Florescentdisplay to display voltage, amperage, air pressure, and the like.Embodiments of the control panel 34 include any number inputs andoutputs, such as welding methods, air compressor settings, oil pressure,oil temperature, and system power. Further, the user inputs 40 andindicators 42 may be electrically coupled to the control circuitry 32and enable a user to set and monitor various parameters within thecontrol circuitry 32 and other devices of the system 10.

The illustrated system 10 also includes various external connections 44.The external connections 44 may include various outlets and couplersconfigured to provide access to the electrical power and the compressedair generated by the system 10. For example, the illustrated externalconnections 44 include an AC power output 46, a DC power output 48, anda compressed air output 50. In an embodiment these outputs 46, 48 and 50are coupled to various devices and tools. For example, the AC poweroutput 46 or the DC power output 48 can be coupled to various weldingand cutting tools 52. As depicted, the welding/cutting tools 52 includeda torch 54 coupled to the external connection 44 via a supply conduit56. For instance, the welding devices may receive current from thegenerator 14 via the external connections 44. In such an embodiment, thetorch 54 may be used to weld or cut a work piece 58 coupled to theexternal connections 44 via a work clamp 60 and a cable 62. As will beappreciated, the torch 54 may include various welding devices, such as aTIG (tungsten inert gas) torch, a MIG (metal inert gas) gun, or a plasmacutting torch. Similarly, the system 10 may provide compressed air fromthe air compressor 16 via the compressed air output 50. For example anair tool 64 may be coupled to the compressed air output 50 via an airhose 66. The air hose 66 may exit the system 10 at various otherlocations; including the back of the system 10 proximate to the aircompressor 16. The air tool 64 may include various pneumatic tools andthe like. In another embodiment, a plasma cutting torch 54 may receivepower from an external unit (e.g., wall outlet AC power) while receivingcompressed air from the air compressor 16 of the system 10.

As discussed previously, the system 10 may include multiple componentsworking in cooperation to generate power, compressed air, and otheroutputs. For example, in the illustrated embodiment, a single engine 12is coupled to the generator 14 and the air compressor 16. As will beappreciated, mechanical design of such a system 10 may entail variousarrangements of components to provide an efficient and reliable system10. For instance, if the components are not positioned correctly withrespect to one another, then the misalignment may cause premature wearand/or failure of the system 10 and its components. For example,misalignment of the stub shaft 22 may reduce the efficiency of thesystem and create additional wear on bearings within the air compressor16 or the engine 12. Further, each of the components may have a tendencyto vibrate and, thus, increase the wear potential on surroundingcomponents. Such a vibration may also reduce the appeal to operators, asthe system 10 may not run as quietly and smoothly as desired. Asdiscussed in further detail below, various features of the system 10 areconfigured to align and isolate components, including the engine 12 andthe air compressor 16.

Turning now to FIG. 4, depicted is a diagram including the engine 12 andthe compressor 14 coupled via the drive belt 30. In an embodiment, asmentioned above, the engine 12 outputs power via the rotating shaft 22and transmit the power to the air compressor 16 via the pulley 24, thedrive belt 30, the compressor pulley 28, and the compressor drive shaft26. For example, as depicted, the engine 12 rotates the drive shaft 22and, in turn, rotates the pulley 24. The rotation of the pulley 24 istransmitted to the compressor pulley 28 via the drive belt 30. Rotationof the compressor drive shaft 26 operates the screw mechanism of therotary screw compressor 16. In other embodiments, the system 10 mayinclude a clutch configured to regulate the transfer of torque from theengine 12 to the compressor 16. For example, clutch mechanism may belocated in-line with the compressor drive shaft 26, in-line with thedrive shaft 22, within the pulley 24, and/or the compressor pulley 28.Accordingly, the engine 12 provides the power to generate compressed airvia the air compressor 16.

In such a system 10, to prevent slipping of the drive belt 30 it isdesirable that the drive belt 30 maintains enough tension to generatefriction between the drive belt 30 and the pulleys 24 and 28.Accordingly, the system 10 may include the belt tensioner 68 configuredto maintain tension and prevent slipping of the drive belt 30. Further,the belt tensioner 68 may provide a simplified method for assembly andmaintenance of the drive belt 30. For instance, the tension of the belt30 may be increased or decreased without an assembler to provide a fulltension when mounting the drive belt 30 to the system 10. In anembodiment, the belt tensioner 68 may provide a biasing force configuredto maintain enough pressure on the drive belt 30 to discourage the drivebelt 30 from slipping on the pulleys 24 and 28.

In one embodiment as shown in FIG. 5, the belt tensioner 68 includes atension pulley 70 configured to contact the drive belt 30 and to providepressure against the drive belt 30. For example, as depicted in FIG. 4,the belt tensioner 68 includes a pivot arm 72 that rotates about a pivotpoint 74 in the direction of arrow 76. In an embodiment, the pivot point74 of the belt tensioner 68 may be coupled to a fixed object, such asthe engine 12, the air compressor 16, or the base/frame 36 via a bolt orother coupling. In the depicted embodiment, the torque to rotate thepivot arm 72 is provided by a torsion spring 78 that is positioned aboutan axis passing through the pivot point 74. Thus, the torque provided bythe torsion spring 78 acts to force the tension pulley 70 to rotate in acounter clockwise direction of the arrow 76 and stretch the drive belt30 to the desired tension.

Similarly, as depicted in FIG. 6, the biasing force to create tensionmay be provided by a linear spring 80 coupled to the pulley 70. Forinstance, linear spring 80 is coupled to the belt tensioner 68 and isconfigured to provide a linear force in the direction of arrow 82. Asfurther depicted, the spring is coupled to a fixed object 84, such asthe engine 12, the air compressor 16, or the base/frame 36. In anotherembodiment, the tensioner 68 may use a pneumatic drive, a hydraulicdrive, or both, to provide the desired force to provide tension in thebelt 30.

The belt tensioner 68 may include any arrangement or device configuredto provide a tension on the drive belt 30. For example the tensionpulley 70 may be located on the outside of the drive belt 30 and providean inward biasing force to provide tension within the drive belt 30.Further, the pivot arm 72 may be manipulated via a torque provided by alinear spring coupled along the length of the pivot arm 72. Otherembodiments may include the use of a linear spring 80 in compressive asopposed to a tensile arrangement.

In another embodiment, the system 10 may include a uniquely resilienttype of the drive belt 30 configured to maintain a tension without theaddition of a belt tensioner 68. For example, the drive belt 30 may bedescribed as a spring belt due to high spring-like characteristics ofthe belt 30. As appreciate, if the distance between the pulleys 24 and28 change due to vibration, movement of the engine 12 and/or thecompressor 16, or other variations, then the resilient or spring-likenature of the belt 30 maintains a sufficient tension as the distanceincreases and subsequently decreases. In other words, the belt 30 maynot permanently stretch out as the distance changes, thereby reducing oreliminating the need for a separate spring-driven tensioner 68. The belt30 may include a rubber belt that is configured to shrink slightly afterand initial use and maintain a tension for the life of the belt, such asthose belts manufactured by Hutchison. Even with such a resilient belt30, the belt tensioner 68 may be incorporated into the system 10 toassist in maintaining tension. However, the use of the belt tensioner 68may not be required to account for stretching of the drive belt 30.

The system 10 may include any belt and pulley arrangement configured totransmit mechanical energy to the air compressor 16. For example, thesystem 10 may include a variety of pulley sizes to provide forappropriate ratios between the drive shaft 22 and the compressor driveshaft 26. For example, if the engine is operating at 4000 rpm and it isdesired that the screw compressor operate at 4000 rpm, the pulley 24 andthe compressor pulley 28 may have approximately the same diameter.However, if the air compressor 16 is configured to operate at 2000 rpm,the compressor pulley 28 may comprise a diameter twice the diameter ofthe pulley 24. Further, an embodiment, the stub shaft 22 may beconfigured to drive multiple devices. For example, the drive belt 30 maybe routed about an additional pulley coupled to another device, such asan additional generator 14, hydraulic motor, or an additional aircompressor 16. Embodiments may also include multiple drive belts 30coupling the stub shaft 22 to multiple devices.

Returning now to the embodiment of FIG. 4, the system 10 may alsoinclude the isolators 86 located between the engine 12 and othercomponents of the system 10, such as the base/frame 36. The isolators 86may include a damping material configured to reduce the transmission ofvibrations from the engine 12 to the base/frame 36 and other componentsof the system 10, such as the air compressor 16. For example, theisolators 86 may comprise a resilient material, such as an elastomer(e.g., rubber), configured to flex slightly under loading caused by theweight and vibration of the engine 12. In other embodiments, theisolators 86 may include damping mechanisms such as springs and shockabsorbers.

Further, the isolators 86 may be configured such that the positioning ofthe engine 12 may change slightly with the addition of pressure to theengine 12 from different directions. In other words, the engineisolators 86 may flex slightly to accommodate for miss-alignments thatcause pressure on different parts of the system 10 and the engine 12.For example, if the stub shaft 22 and the compressor drive shaft 26 arenot parallel, then the isolators 86 may flex slightly to relieve anypressure that may be applied to the stub shaft 22. These may includepressures that are due to the drive belt 30 tension pulling the shafts22 and 26 into alignment. Accordingly, the isolators 86 may aid inpreventing premature wear of the components, such as bearings, of thesystem 10.

Further, the isolators 86 may be used to couple the engine 12 to theother components of the system 12. In an embodiment, the isolators 86may include features configured to attach the engine 12 to thebase/frame 36. For example, the isolators 86 may include an attachmentfeature, such as a bolt stud formed into the body of the isolator 86 andcoupled to the engine 12 and the base/frame 36. Other embodiments mayinclude passing a fastening mechanism, such as a bolt, through the bodyof the isolator 86. In an embodiment, the isolators 86 may include adisk of material that is compressed between the engine 12 and thebase/frame 36. For example, the engine 12 may be mounted to thebase/frame 36 via a bolt, and the isolators 86 may be compressed theengine 12 and the base/frame 36 via the tightening of the bolt. As willbe appreciated, the biasing force of the isolators 86 may also act as awasher by providing a continuous pressure to prevent the bolt frombacking out of the mating threads. In an embodiment, multiple isolators86 may be located under the engine 12, such as four isolators 86 mountednear the corners of the engine 12. In an embodiment, the system 10 maycomprise only a single isolator 86 located under the engine 12. Forexample, the isolator 86 may comprise a single sheet of material locatedbetween the engine 12 and the other components of the system 10.

In other embodiments, one or more isolators 86 (e.g., resilient mounts)may be used to couple the engine 12, the generator 14, or the compressor16, or any combination thereof, to the frame 36. However, the compressor16 remains separate from the engine 12 and the compressor 16 isindependently mounted to the frame 36. Again, in one embodiment, thecompressor 16 is rigidly coupled to the frame 36 without the one or moreisolators 86, and the engine 12 is resiliently coupled to the frame 36with the one or more isolators 86. The one or more isolators 86 may beconfigured to dampen vibrations, expand and compress to maintainalignment between the engine 12 and the compressor 16, or a combinationthereof.

The system 10 may also include a bearing that has characteristicsbeneficial to loading that may be experienced within the system 10. Oneembodiment of the bearing may include an aluminum journal bearingconfigured to support the loads experienced by the shaft 22 or thecompressor drive shaft 26. In other embodiments, a bearing may includematerials with increased hardness, such as bronze or brass. The bearingmay be located within the engine 12 to support the shaft 20 and 22,and/or may be located within the compressor 16 to support the compressordrive shaft 26. Accordingly, increased hardness within the bearing mayhelp to resist wear that may otherwise be present due to the loadingbetween the shafts 22 and 26.

While only certain features of the invention have been illustrated anddescribed herein, many modifications and changes will occur to thoseskilled in the art. It is, therefore, to be understood that the appendedclaims are intended to cover all such modifications and changes as fallwithin the true spirit of the invention.

1. A system, comprising: a chassis; an engine coupled to the chassis; agenerator coupled to the engine; a compressor coupled to the chassisindependent from the engine, wherein the engine is configured to driveboth the generator and the compressor; and a geometrically adjustablecoupling disposed between a first shaft of the engine and a second shaftof the compressor, wherein the geometrically adjustable coupling isconfigured to maintain a connection between the first and second shaftsduring relative movement between the engine and the compressor.
 2. Thesystem of claim 1, wherein the geometrically adjustable couplingcomprises a resilient belt configured to expand and contract withvariations in distance between the first shaft and the second shaft,while maintaining tension.
 3. The system of claim 1, wherein thegeometrically adjustable coupling comprises an adjustable tensionerconfigured to bias a belt or a chain.
 4. The system of claim 3, whereinthe adjustable tensioner comprises a tension pulley configured tocontact the belt or chain and provide pressure against the belt orchain.
 5. The system of claim 4, wherein the tension pulley is coupledto a pivot arm biased to rotate about a pivot point by a torsion spring.6. The system of claim 4, wherein the tension pulley is coupled to alinear spring configured to bias the tension pulley against the belt orchain.
 7. The system of claim 3, wherein the adjustable tensionercomprises a spring.
 8. The system of claim 7, comprising a first pulleycoupled to the first shaft, a second pulley coupled to the second shaft,and the belt or the chain disposed in tension about the first and secondpulleys.
 9. The system of claim 1, comprising one or more resilientmounts coupling the engine, or the generator, or the compressor, or anycombination thereof, to the chassis with the compressor separate fromthe engine and the generator.
 10. The system of claim 9, wherein the oneor more resilient mounts are configured to dampen vibrations, expand andcompress to maintain alignment between the engine and the compressor, ora combination thereof.
 11. The system of claim 9, wherein the compressoris rigidly coupled to the chassis without the one or more resilientmounts, and the engine is resiliently coupled to the chassis with theone or more resilient mounts.
 12. The system of claim 9, wherein the oneor more resilient mounts comprise an elastomer.
 13. The system of claim9, wherein the one or more resilient mounts comprise one or moresprings.
 14. A method, comprising: isolating an air compressor from anengine and a generator in a common chassis, wherein isolating comprisesseparately mounting the air compressor and the engine with a resilientor distance adjustable connection, and isolating comprises resilientlymounting the engine, or the air compressor, or both, to a chassis. 15.The method of claim 14, wherein the resilient or distance adjustableconnection comprises an adjustable tensioner configured to bias a beltor a chain.
 16. The method of claim 15, wherein the adjustable tensionercomprises a tension pulley configured to contact the belt or chain andprovide pressure against the belt or chain.
 17. The method of claim 16,wherein the tension pulley is coupled to a pivot arm biased to rotateabout a pivot point by a torsion spring.
 18. The method of claim 16,wherein the tension pulley is coupled to a linear spring configured tobias the tension pulley against the belt or chain.
 19. The method ofclaim 14, wherein the resilient or distance adjustable connectioncomprises a resilient belt configured to expand and contract withvariations in distance between the air compressor and the engine, whilemaintaining tension.
 20. The method of claim 19, wherein the resilientbelt comprises a spring belt having spring-like resilient properties.